FDS Source: Rework velocity BC at corners

Author: mcgratta

Source/velo.f90

@@ -2326,23 +2326,24 @@ SUBROUTINE VELOCITY_BC(T,NM,APPLY_TO_ESTIMATED_VARIABLES)
 
                CASE (WALL_MODEL_BC) BOUNDARY_CONDITION
 
-                  ITMP = MIN(I_MAX_TEMP,NINT(0.5_EB*(TMP(IIGM,JJGM,KKGM)+TMP(IIGP,JJGP,KKGP))))
-                  MU_WALL = MU_RSQMW_Z(ITMP,1)/RSQ_MW_Z(1)
-                  RHO_WALL = 0.5_EB*( RHOP(IIGM,JJGM,KKGM) + RHOP(IIGP,JJGP,KKGP) )
-
-                  CALL WALL_MODEL(SLIP_COEF,U_TAU,Y_PLUS,MU_WALL/RHO_WALL,SF%ROUGHNESS,0.5_EB*DXX(ICD),VEL_GAS-VEL_T)
-
                   ! SLIP_COEF = -1, no slip,   VEL_GHOST = 2*VEL_T - VEL_GAS
                   ! SLIP_COEF =  0, half slip, VEL_GHOST = VEL_T
                   ! SLIP_COEF =  1, free slip, VEL_GHOST = VEL_GAS
 
-                  IF ((IWM==0.OR.IWP==0) .AND. .NOT.ED%EXTERNAL) SLIP_COEF = 0._EB  ! Corner
-                  VEL_GHOST = VEL_T + SLIP_COEF*(VEL_GAS-VEL_T)
-                  DUIDXJ(ICD_SGN) = I_SGN*(VEL_GAS-VEL_GHOST)/DXX(ICD)
-                  MU_DUIDXJ(ICD_SGN) = RHO_WALL*U_TAU**2 * SIGN(1._EB,DUIDXJ(ICD_SGN))
+                  IF ((IWM==0.OR.IWP==0) .AND. .NOT.ED%EXTERNAL) THEN  ! Special case for a corner
+                     VEL_GHOST = 2._EB*VEL_T - VEL_GAS
+                     DUIDXJ(ICD_SGN) = I_SGN*(VEL_GAS-VEL_GHOST)/DXX(ICD)
+                     MU_DUIDXJ(ICD_SGN) = MUA*DUIDXJ(ICD_SGN)
+                  ELSE
+                     ITMP = MIN(I_MAX_TEMP,NINT(0.5_EB*(TMP(IIGM,JJGM,KKGM)+TMP(IIGP,JJGP,KKGP))))
+                     MU_WALL = MU_RSQMW_Z(ITMP,1)/RSQ_MW_Z(1)
+                     RHO_WALL = 0.5_EB*( RHOP(IIGM,JJGM,KKGM) + RHOP(IIGP,JJGP,KKGP) )
+                     CALL WALL_MODEL(SLIP_COEF,U_TAU,Y_PLUS,MU_WALL/RHO_WALL,SF%ROUGHNESS,0.5_EB*DXX(ICD),VEL_GAS-VEL_T)
+                     VEL_GHOST = VEL_T + SLIP_COEF*(VEL_GAS-VEL_T)
+                     DUIDXJ(ICD_SGN) = I_SGN*(VEL_GAS-VEL_GHOST)/DXX(ICD)
+                     MU_DUIDXJ(ICD_SGN) = RHO_WALL*U_TAU**2 * SIGN(1._EB,DUIDXJ(ICD_SGN))
+                  ENDIF
                   ALTERED_GRADIENT(ICD_SGN) = .TRUE.
-                  ! After stress and velocity gradient have been computed, reset VEL_GHOST to NO_SLIP for visualizaiton
-                  ! VEL_GHOST = 2._EB*VEL_T - VEL_GAS
 
                CASE (BOUNDARY_FUEL_MODEL_BC) BOUNDARY_CONDITION
 

Utilities/Matlab/FDS_verification_dataplot_inputs.csv

@@ -480,8 +480,8 @@ d,Morvan_TGA,WUI/Morvan_TGA_git.txt,WUI/Morvan_Data_Mass.csv,1,2,T (C),Normalize
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@@ -773,7 +773,7 @@ d,zone_break_fast,Pressure_Effects/zone_break_fast_git.txt,Pressure_Effects/zone
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